View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 21015U 90111B 25132.45989265 .00000277 00000-0 10191-3 0 9993
2 21015 74.0503 241.5759 0021015 154.0529 206.1683 14.37072157900235
| Epoch (UTC): | 12 May 2025 11:02:14 |
| Eccentricity: | 0.0021015 |
| inclination: | 74.0503° |
| perigee height: | 753 km |
| apogee height: | 783 km |
| right ascension of ascending node: | 241.5759° |
| argument of perigee: | 154.0529° |
| revolutions per day: | 14.37072157 |
| mean anomaly at epoch: | 206.1683° |
| orbit number at epoch: | 90023 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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